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1 SVENSK STANDARD SS-EN 4471:2007 Fastställd Utgåva 1 Aerospace series Steel FE-PM1505 (X1CrNiMoAITi12-9-2) Vacuum induction melted and consumable electrode remelted and precipitation treated Forgings - a or D 150 mm - Rm MPa ICS Språk: engelska Publicerad: september 2007 Copyright SIS. Reproduction in any form without permission is prohibited.

2 Europastandarden EN 4471:2007 gäller som svensk standard. Detta dokument innehåller den officiella engelska versionen av EN 4471:2007. The European Standard EN 4471:2007 has the status of a Swedish Standard. This document contains the official English version of EN 4471:2007. Upplysningar om sakinnehållet i standarden lämnas av SIS, Swedish Standards Institute, telefon Standarder kan beställas hos SIS Förlag AB som även lämnar allmänna upplysningar om svensk och utländsk standard. Postadress: SIS Förlag AB, STOCKHOLM Telefon: Telefax: E-post: sis.sales@sis.se. Internet:

3 EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM EN 4471 July 2007 ICS English Version Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) - Vacuum induction melted and consumable electrode remelted - and precipitation treated - Forgings - a or D 150 mm - Rm MPa Série aérospatiale - Acier FE-PM1505 (X1CrNiMoAlTi ) - Élaboré sous vide par induction et refondu à l'électrode consommable - Mis en solution et vieilli - Pièces forgées et pièces matricées - a ou D 150 mm - Rm MPa Luft- und Raumfahrt - Stahl FE-PM1505 (X1CrNiMoAlTi12-9-2) - Vakuuminduktionserschmolzen und mit selbstverzehrende Elektrode umgeschmolzen - Lösungsgeglüht und ausgelagert - Schmiedestücke - a oder D 150 mm - Rm MPa This European Standard was approved by CEN on 15 February CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN Management Centre or to any CEN member. This European Standard exists in three official versions (English, French, German). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the CEN Management Centre has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG Management Centre: rue de Stassart, 36 B-1050 Brussels 2007 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4471:2007: E

4 EN 4471:2007 (E) Provläsningsexemplar / Preview Foreword This document (EN 4471:2007) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of the member countries of ASD, prior to its presentation to CEN. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by January 2008, and conflicting national standards shall be withdrawn at the latest by January Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN [and/or CENELEC] shall not be held responsible for identifying any or all such patent rights. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. 2

5 EN 4471:2007 (E) Introduction This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN This standard has been prepared in accordance with EN Scope This standard specifies the requirements relating to: for aerospace applications. Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) Vacuum induction melted and consumable electrode remelted and precipitation treated Forgings a or D 150 mm R m MPa 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 4258, Aerospace series Metallic materials General organization of standardization Links between types of EN standards and their use. EN 4346, Aerospace series Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) Vacuum induction melted and consumable electrode remelted Softened Forging stock a or D 300 mm. 1) EN , Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 5: Specific rules for steels. 1) EN , Aerospace series Steel and heat resisting alloys Wrought products Technical specification Part 6: Pre-production and production forgings. 2) 1) Published as ASD Prestandard at the date of publication of this standard. 2) In preparation at the date of publication of this standard. 3

6 EN 4471:2007 (E) 1 Material designation Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) 2 Chemical composition % Element C Si Mn P S Cr Mo Ni Al Ti N 2 Fe min. 11,50 1,85 8,50 0,60 0,28 Base max. 0,015 0,10 0,10 0,010 0,005 12,50 2,15 9,50 0,80 0,37 0,010 3 Method of melting Vacuum induction melted and consumable electrode remelted 4.1 Form Forgings 4.2 Method of production Forged from forging stock EN Limit dimension(s) mm a or D Technical specification EN Delivery condition Heat treatment 820 C θ 860 C / OQ, AQ or WQ + cooling to θ 20 C and precipitation treated 820 C θ 860 C / OQ, AQ or WQ + cooling to θ 20 C C θ 545 C / t 4 h / AC 6.2 Delivery condition code W U 7 Use condition and precipitation treated Delivery condition Heat treatment C θ 545 C / t 4 h / AC Characteristics 8.1 Test sample(s) See EN Test piece(s) See EN Heat treatment Delivery condition Use condition 9 Dimensions concerned mm a or D 150 a or D 150 a 75 a or D Thickness of cladding on each face % 11 Direction of test piece L T 12 Temperature θ C Ambient Ambient 13 Proof stress R p0,2 MPa T Strength R m MPa Elongation A % Reduction of area Z % Hardness 363 HB 380 HB 380 HB 18 Shear strength R c MPa 19 Bending k 20 Impact strength KV 50 J ; Notch direction T + KV 20 J, at 40 C ; Notch direction T 21 Temperature θ C KV 40 J ; Notch direction L + KV 15 J, at 40 C ; Notch direction L 22 Time h 23 Stress σ a MPa C 24 Elongation a % 25 Rupture stress σ R MPa 26 4 Elongation at rupture A % 27 Notes (see line 98) a